GB1102792A - Alternator tachometer - Google Patents
Alternator tachometerInfo
- Publication number
- GB1102792A GB1102792A GB6871/65A GB687165A GB1102792A GB 1102792 A GB1102792 A GB 1102792A GB 6871/65 A GB6871/65 A GB 6871/65A GB 687165 A GB687165 A GB 687165A GB 1102792 A GB1102792 A GB 1102792A
- Authority
- GB
- United Kingdom
- Prior art keywords
- voltage
- primary
- current
- potential
- core
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
- G01P3/42—Devices characterised by the use of electric or magnetic means
- G01P3/44—Devices characterised by the use of electric or magnetic means for measuring angular speed
- G01P3/46—Devices characterised by the use of electric or magnetic means for measuring angular speed by measuring amplitude of generated current or voltage
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
- Indication And Recording Devices For Special Purposes And Tariff Metering Devices (AREA)
- Control Of Eletrric Generators (AREA)
Abstract
1,102,792. Measuring speed of internal combustion engines, electrically. STEWARTWARNER CORPORATION. Feb.17, 1965 [Feb.17, 1964], No.6871/65. Heading G1N. A tachometer (e.g. for an automobile engine) comprises a saturable transformer 72 (Fig. 2) the primary 74 of which is connected between an A. C . potential source (terminal 64), from an alternator 42 driven by the engine, and a D.C. bias potential at end 74b, and a meter 70 is connected to measure the time average secondary current as a function of speed. The alternator 42 charges a storage battery 50 through a three phase bridge rectifier network. One end of the primary 74 is connected via a resistor 78a to a positive D.C. potential at 58 and to earth via a resistor 78b so that the potential at terminal 64 fluctuates between earth potential and a positive potential approximating the voltage at 58 (Fig. 3a). In operation, with the transformer core saturated in say a negative direction the primary current wave (Fig.3b) follows the increasing voltage (Fig. 3a) and increases until at point X it causes the core flux density to drop below saturation level and the inductance of the winding therefore increases causing the current to level off. The core flux changes direction until at point Y it reaches saturation in the opposite or positive direction, where at the inductance being negligible the current again increases until it attains a level determined by the limiting resistors 78a, 78b. When the voltage at terminal 64 swings from earth potential in a positive direction relative to the voltage at the opposite end of the primary, the core is driven to saturation in one direction, and when the voltage at 64 swings in a negative direction the primary current reverses and the respective saturation points of the core are indicated at X' and Y' on Fig. 3b. The voltage induced in the secondary winding is shown in Fig. 3c, and follows the primary voltage during the periods X to Y and X' to Y' &c., when the core is not saturated. The secondary voltage is thus a function of the primary current and of the saturation time. The current output of the secondary across a portion of a potentiometer 91 is shown (Fig. 3d) and the average voltage drop thereacross is a function of the frequency of the pulses. By virtue of its mechanical inertia the meter 70 measures average current through it and is calibrated to indicate speed. An NTC resistor 98 may be provided in the secondary circuit to provide temperature compensation.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US345354A US3314007A (en) | 1964-02-17 | 1964-02-17 | Alternator operated tachometer circuit |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1102792A true GB1102792A (en) | 1968-02-07 |
Family
ID=23354719
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6871/65A Expired GB1102792A (en) | 1964-02-17 | 1965-02-17 | Alternator tachometer |
Country Status (3)
Country | Link |
---|---|
US (1) | US3314007A (en) |
DE (1) | DE1523254A1 (en) |
GB (1) | GB1102792A (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3891925A (en) * | 1973-12-03 | 1975-06-24 | Nasa | Tachometer circuit |
US4439721A (en) * | 1982-02-12 | 1984-03-27 | Outboard Marine Corporation | Magneto alternator regulator with tachometer output |
CA2112636A1 (en) * | 1993-12-30 | 1995-07-01 | Normand Dery | Remote starting system for a vehicle having a diesel engine |
US20020129613A1 (en) * | 2000-10-10 | 2002-09-19 | Thermo King Corporation | Cryogenic refrigeration unit suited for delivery vehicles |
US6751966B2 (en) * | 2001-05-25 | 2004-06-22 | Thermo King Corporation | Hybrid temperature control system |
US6609382B2 (en) * | 2001-06-04 | 2003-08-26 | Thermo King Corporation | Control method for a self-powered cryogen based refrigeration system |
US6631621B2 (en) * | 2001-07-03 | 2003-10-14 | Thermo King Corporation | Cryogenic temperature control apparatus and method |
US6698212B2 (en) * | 2001-07-03 | 2004-03-02 | Thermo King Corporation | Cryogenic temperature control apparatus and method |
US6694765B1 (en) * | 2002-07-30 | 2004-02-24 | Thermo King Corporation | Method and apparatus for moving air through a heat exchanger |
US6895764B2 (en) * | 2003-05-02 | 2005-05-24 | Thermo King Corporation | Environmentally friendly method and apparatus for cooling a temperature controlled space |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3044013A (en) * | 1959-05-06 | 1962-07-10 | United Aircraft Corp | Three-phase voltage responsive speed sensor |
US2972107A (en) * | 1960-01-04 | 1961-02-14 | Bendix Corp | Voltage sensitive timing device |
-
1964
- 1964-02-17 US US345354A patent/US3314007A/en not_active Expired - Lifetime
-
1965
- 1965-02-10 DE DE19651523254 patent/DE1523254A1/en active Pending
- 1965-02-17 GB GB6871/65A patent/GB1102792A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE1523254A1 (en) | 1969-04-03 |
US3314007A (en) | 1967-04-11 |
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